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Aircraft has high-lift system that is arranged on wing of aircraft and comprises drive unit for converting electrical energy into speed-controlled rotary motion, where energy storage device is assigned to high-lift system for its actuation
Aircraft has high-lift system that is arranged on wing of aircraft and comprises drive unit for converting electrical energy into speed-controlled rotary motion, where energy storage device is assigned to high-lift system for its actuation
The aircraft has a high-lift system, which is arranged on a wing (10) of the aircraft and comprises a drive unit for converting electrical or hydraulic energy into a speed-controlled rotary motion, and a control unit for controlling the high-lift system. An energy storage device is assigned to the high-lift system for its actuation. The drive unit is connected with the energy storage device. A flap (12,14) of the high-lift system has multiple separate actuators (16,18,20,22). The energy storage device is a hydraulic storage device.
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